In an aerospace environment, mitigation strategies may be needed to ensure reliable and safe operation of an electronic device (e.g., a processor). If the device gets too hot (e.g., reaches a temperature that exceeds a threshold), the operation of the device may be degraded or even cease altogether.
It can be difficult to implement mitigation strategies in an aerospace environment. For example, a lack of space and airflow might not allow a fan to be used to cool a device. Further complicating matters is the fact that a first instance of the device may vary from a second instance of the device due to an allowable tolerance in materials or fabrication processes used to manufacture the device.
An embodiment is directed to an apparatus comprising: a thermal block coupled to an electronic device, a thermal strap coupled to the thermal block, and retention hardware coupled to the thermal strap and configured to retain the thermal block within the thermal strap when the apparatus is exposed to at least one variable environmental condition.
An embodiment is directed to a method comprising: coupling a thermal strap and a thermal block, coupling retention hardware configured to retain the thermal block within the thermal strap when the apparatus is exposed to at least one variable environmental condition and the thermal block, and coupling the thermal block to an electronic device.
Additional embodiments are described below.
The present disclosure is illustrated by way of example and not limited in the accompanying figures in which like reference numerals indicate similar elements.
It is noted that various connections are set forth between elements in the following description and in the drawings (the contents of which are included in this disclosure by way of reference). It is noted that these connections in general and, unless specified otherwise, may be direct or indirect and that this specification is not intended to be limiting in this respect. In this respect, a coupling between entities may refer to either a direct or an indirect connection.
Exemplary embodiments of apparatuses, systems, and methods are described for mitigating the impact of environmental conditions on the availability and functionality of a device, such as a processor. In some embodiments, the device may be associated with an engine or airframe of an aircraft. In some embodiments, an assembly may include adjustment or retention hardware and a block that are configured to mitigate or avoid applications of stress to the device. The assembly may include a spring to control a load that may be placed on the device. The assembly may include a strap that may conduct heat away from the device.
Referring to
In some embodiments, the device (e.g., the processor) may be subject to one or more tolerances, such that a configurable or flexible assembly may be needed. In other words, simply applying a fixed-configuration strap 102 to the device could result in a substantial risk of damage to the device. In this respect, a thermal block 116 may be used. The block 116 may float within a cutout 124 of the strap 102 such that the device will not be crushed or damaged. The block 116 may float while the strap 102, which may include one or more posts, is fastened or coupled to the heat sink or to the housing. The block 116 is also used to provide thermal conduction between, e.g., the device and the strap 102.
Referring now to
Referring now to
When a technician or operator is putting together or constructing the assembly 300, it is possible that the operator might be inclined to press down on, or apply pressure to, the top of the block 116. This application of pressure, if not controlled, may be sufficient to damage or crack (the die of) the device 352.
Referring now to
In operation 502, a strap (e.g., strap 102) and a block (e.g., block 116) may be coupled to one another.
In operation 504, a spring (e.g., spring 456) and the block may be coupled to one another.
In operation 506, retention hardware (e.g., retention hardware 230) and the block 506 may be coupled to one another.
In operation 508, the block and a pad (e.g., pad 340) may be coupled to one another.
In operation 510, the pad and a device (e.g., device 352) may be coupled to one another.
The method 500 is illustrative. In some embodiments, one or more of the operations may be optional. In some embodiments, additional operations not shown may be included. In some embodiments, the operations may execute in an order or sequence that is different from what is shown in
As described herein, in some embodiments various functions or acts may take place at a given location and/or in connection with the operation of one or more apparatuses, systems, or devices. For example, in some embodiments, a portion of a given function or act may be performed at a first device or location, and the remainder of the function or act may be performed at one or more additional devices or locations.
Aspects of the disclosure have been described in terms of illustrative embodiments thereof Numerous other embodiments, modifications and variations within the scope and spirit of the appended claims will occur to persons of ordinary skill in the art from a review of this disclosure. For example, one of ordinary skill in the art will appreciate that the steps described in conjunction with the illustrative figures may be performed in other than the recited order, and that one or more steps illustrated may be optional.
This invention was made with Government support with the United States Air Force under contract No. N00019-02-C-3003. The Government has certain rights in this invention.